1. An iterative analytical technique for the design of interplanetary direct transfer trajectories including perturbations. Issue 12 (15th June 2018) Authors: Parvathi, S.P.; Ramanan, R.V. Journal: Advances in space research Issue: Volume 61:Issue 12(2018) Page Start: 3002 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
2. Direct transfer trajectory design options for interplanetary orbiter missions using an iterative patched conic method. Issue 7 (1st April 2017) Authors: Parvathi, S.P.; Ramanan, R.V. Journal: Advances in space research Issue: Volume 59:Issue 7(2017) Page Start: 1763 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
3. Fuel-optimal and Energy-optimal guidance schemes for lunar soft landing at a desired location. Issue 6 (15th March 2021) Authors: Remesh, N.; Ramanan, R.V.; Lalithambika, V.R. Journal: Advances in space research Issue: Volume 67:Issue 6(2021) Page Start: 1787 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
4. Precise halo orbit design and optimal transfer to halo orbits from earth using differential evolution. Issue 1 (1st January 2016) Authors: Nath, Pranav; Ramanan, R.V. Journal: Advances in space research Issue: Volume 57:Issue 1(2016) Page Start: 202 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗